Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2.05, 2.54, and 2.04
Publisher: NACA
Published: 1952
Place of publication: Washington, D.C.
Language: eng
Number of pages: 20
Subjects: Aerodynamics--Research; Drag (Aerodynamics.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003809150&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003809150&ix=nu&I=0&V=D&pm=1</a>